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    Titel :

    AIAA-2005-1058 BOUNDARY LAYER DEVELOPMENT ON ROTOR BLADES OF A FOUR-STAGE LOW-SPEED AXIAL COMPRESSOR



    Kongress:

    17th, International symposium on air breathing engines ; 2005 ; Munich, Germany



    Erscheinungsdatum :

    2005-01-01


    Format / Umfang :

    43 pages


    Anmerkungen:

    Includes bibliographical references and index; Papers on CD-ROM



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    AIAA-2005-1221 FIRST STAGE OF THE CENTRIFUGAL COMPRESSOR DESIGN WITH TANDEM ROTOR BLADES

    Hanus, D. / Censky, T. / Neveceral, J. et al. | British Library Conference Proceedings | 2005


    AIAA-2005-1184 AERODYNAMIC STUDIES ON SWEPT BLADES FOR AXIAL FLOW FAN/COMPRESSOR

    Roy, B. / Chouhan, M. / American Institute of Aeronautics and Astronautics; International Society for Air Breathing Engines | British Library Conference Proceedings | 2005



    AIAA-2005-1096 TIP-CLEARANCE VARIATIONS OF AN AXIAL HIGH-SPEED SINGLE-STAGE TRANSONIC COMPRESSOR

    Bergner, J. / Hennecke, D.K. / Hah, C. et al. | British Library Conference Proceedings | 2005


    AIAA-2005-1181 AUTOMATIC MULTI-STAGE DESIGN / OPTIMIZATION OF AN AXIAL COMPRESSOR

    Benito, D. / Shahpar, S. / American Institute of Aeronautics and Astronautics; International Society for Air Breathing Engines | British Library Conference Proceedings | 2005